DE2733443A1 - Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas - Google Patents

Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

Info

Publication number
DE2733443A1
DE2733443A1 DE19772733443 DE2733443A DE2733443A1 DE 2733443 A1 DE2733443 A1 DE 2733443A1 DE 19772733443 DE19772733443 DE 19772733443 DE 2733443 A DE2733443 A DE 2733443A DE 2733443 A1 DE2733443 A1 DE 2733443A1
Authority
DE
Germany
Prior art keywords
aluminum
gas
exhaust gas
internal combustion
silencer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
DE19772733443
Other languages
German (de)
Inventor
Hans Karl Dr Leistritz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from DE19772719634 external-priority patent/DE2719634A1/en
Application filed by Individual filed Critical Individual
Priority to DE19772733443 priority Critical patent/DE2733443A1/en
Priority to DE19772747655 priority patent/DE2747655A1/en
Priority to IT22649/78A priority patent/IT1095302B/en
Priority to JP4868178A priority patent/JPS5416041A/en
Priority to GB16521/78A priority patent/GB1603962A/en
Priority to US05/900,247 priority patent/US4233812A/en
Priority to BE187201A priority patent/BE866483A/en
Priority to FR7812561A priority patent/FR2388993A1/en
Publication of DE2733443A1 publication Critical patent/DE2733443A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/18Construction facilitating manufacture, assembly, or disassembly
    • F01N13/1838Construction facilitating manufacture, assembly, or disassembly characterised by the type of connection between parts of exhaust or silencing apparatus, e.g. between housing and tubes, between tubes and baffles
    • F01N13/1844Mechanical joints
    • F01N13/1855Mechanical joints the connection being realised by using bolts, screws, rivets or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/003Silencing apparatus characterised by method of silencing by using dead chambers communicating with gas flow passages
    • F01N1/006Silencing apparatus characterised by method of silencing by using dead chambers communicating with gas flow passages comprising at least one perforated tube extending from inlet to outlet of the silencer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/02Silencing apparatus characterised by method of silencing by using resonance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N1/00Silencing apparatus characterised by method of silencing
    • F01N1/02Silencing apparatus characterised by method of silencing by using resonance
    • F01N1/023Helmholtz resonators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/16Selection of particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/02Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/02Exhaust treating devices having provisions not otherwise provided for for cooling the device
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2450/00Methods or apparatus for fitting, inserting or repairing different elements
    • F01N2450/24Methods or apparatus for fitting, inserting or repairing different elements by bolts, screws, rivets or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/02Tubes being perforated
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/10Tubes having non-circular cross section
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/18Structure or shape of gas passages, pipes or tubes the axis of inlet or outlet tubes being other than the longitudinal axis of apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2470/00Structure or shape of gas passages, pipes or tubes
    • F01N2470/26Tubes being formed by extrusion, drawing or rolling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/14Dead or resonance chambers connected to gas flow tube by relatively short side-tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/15Plurality of resonance or dead chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2490/00Structure, disposition or shape of gas-chambers
    • F01N2490/15Plurality of resonance or dead chambers
    • F01N2490/155Plurality of resonance or dead chambers being disposed one after the other in flow direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

A silencer forming part of the exhaust system of an internal combustion engine consists of two concentric tubes (51, 52). These tubes are joined by radial walls (55) which extend longitudinally so that the annular space between the tubes is divided into a number of separate compartments (5). A cooling fluid flows in these compartments (5) in the opposite direction to the flow of gas in the central bore (50). The outer wall of the outer tube (52) has a number of radial fins (56) which also extend longitudinally. These fins help to dissipate the heat which has been transferred to the cooling medium by convection and radiation.

Description

Zusatzanmeldung zur Patentanmeldung P 27 19 634.5 (lei S 773)Additional application to patent application P 27 19 634.5 (lei S 773)

Bezeichnung der Zusatzanmeldung : "Thermische Abgasführung Zusatz 6" Beschreibung In der Patentanmeldung P 27 19 634.5, welche die Bezeichnung trägt "Thermische Abgasführung Zusatz 1", azurde das aluminiumgefertigte Bauelement eines ilohikammerringrohres in Abgasanlagen von Brennkraftmaschinen aus der Technologie einer thermischen Gasführung integriert, deren Gesichtspunkte erstens darin bestehen, jeder Heißgasbeaufschlagung einer Aluminiumwandung zur jenseitigen Oberfläche derselben Wandung ein thermisches Gefälle zuzuordnen, und zweitens darin, den lfeißgaseinlauf in das Gerät in der Vorzone, womit jede Zone vor der Beaufschlagung von Aluminiumwandungen bezeichnet wird, einem Wärmeentzug zu unterwerfen. Letzteres war der Gegenstand der Ansprüche 4 und 5 und hinsichtlich der die Bevchreibung unterstützenden Schemazeichnungen Gegenstand der Figuren 4 und 6. Diese Zusatzanmeldung hat die Aufgabe, einerseits die in der Beschreibung von P 27 19 634.5 offenbarten Erfindungsgedanken bezüglich der Anspruchsfassung noch genauer zu konkretisieren und andererseits weitere konstruktive Gesichtspunkte hinzuzufügen. Aus diesem Grunde werden die Zeichnungen 4 und 6 von P 27 19 634.5 hier als Figuren 2 und 3 unverändert wiederholt. Der Neuheitsgehalt dieser Anmeldung ist infolgedessen mit Figur 1 näher erläutert.Designation of the additional application: "Thermal exhaust gas routing addition 6 "Description In the patent application P 27 19 634.5, which bears the designation "Thermal exhaust gas routing additive 1", azurde the aluminum-made component of a ilohikammerringrohres in exhaust systems of internal combustion engines from the technology integrated into a thermal gas flow, the aspects of which are firstly, each hot gas application of an aluminum wall to the opposite surface of the same Wall to assign a thermal gradient, and secondly, to assign the hot gas inlet into the device in the pre-zone, which means that each zone is in front of the impact of aluminum walls is designated to subject to a heat extraction. The latter was the subject of claims 4 and 5 and with regard to the schematic drawings supporting the description Subject of Figures 4 and 6. This additional application has the task on the one hand relating to the inventive ideas disclosed in the description of P 27 19 634.5 the claim formulation to be more precise and, on the other hand, further constructive ones To add points of view. For this reason, drawings 4 and 6 of P 27 19 634.5 repeated here unchanged as Figures 2 and 3. The novelty content this application is consequently explained in more detail with FIG.

Die Figuren 2 und 3 besitzen die oben geschilderte "Vorzone" in den gleichlautend mit 17 bezeichneten Räumen, in welche der Heißgaseinlau£ beide Nale aus den Lochungen 18 erfolgt. Diese Vorzonen 17 werden, wie in beiden Figuren dargestellt, von den aus den Aluminumteilen das Abgas herausführenden Rohren 16 durchquert. Da diese Rohre 16 nach ihrem Durchlauf durch die stark Wärme aufnehmenden Aluminumwandungen ein Abgas wesentlich tieferer Temperatur besitzen, erfolgt aus den Vorzonen 17 eine ständige Wärmeabgabe im Wärmetausch zu diesen Austrittsrohren 16. Diese bereits in P 27 19 634.5 dargestellte Konstruktion, dem Heißgas der Vorzonen gleichsam im Kurzschlußwege unter Umgehung der Aluminumbauteile im Wärmetausch direkt Richtung Gerätaustritt Wärme zu entziehen, wird in der Figur 1 dieser Zusatzanmeldung für den Anwendungsfall dargestellt, daß die Vorzone nicht wie in den Figuren 2 und 3 im hinteren Teil der Abgasanlage angeordnet sind, sondern im vorderen Teil. Der technologische Inhalt der bezeichneten Aussage wird hierdurch nicht verändert. In allen drei Fällen erfolgt im Wärmetausch eine direkte Wärme zulieferung aus der Vorzone in Richtung Gerätaustritt unter Überspringung der Aluminumteile. In Fig ur 1 ist der Raum 4 die das Heißgas in die Aluminumteile zuliefernde Vorzone. Das in der Konstruktion Figur 1 enthaltene Aluminiumbauteil ist ein stranggepreßtes Rohr mit den Gasführungskanalgruppen 14, 12 und 11 (von außen nach innen aufgezählt). In seinem Inneren wird der Gasführungsraum 11 durch das in der Regel nicht aus Aluminum gefertigte Rohr 16 durchquert, das zugleich Austrittsrohr des Abgases in die freie Atmosphäre darstellt. Aus den Teilstromgruppen 14 läuft das Abgas über den thermisch abkühlenden Zwischenraum 10 durch die Leitung 11 und die Lochungen 15 in den Kegelinnenraum 18, der mit seiner Wandung 19 im Wärmetausch zur Heißgaszone 4 steht, und zwar mit sehr großer Oberfläche. Die nunmehr durch das Rohr 16 dem Austritt zugeführte Wärmemenge entlastet die Abgasführungen, die ganz oder teilweise Aluminumwandungen aufweisen.Figures 2 and 3 have the "pre-zone" described above in the Identically designated with 17 rooms, in which the hot gas inlet £ both channels from the holes 18 takes place. These pre-zones 17 are, as shown in both figures, of the pipes 16 leading out of the aluminum parts, traversed by the exhaust gas. There these tubes 16 after they have passed through the aluminum walls, which absorb a great deal of heat an exhaust gas is essential have a lower temperature, takes place from the Prezones 17 a constant release of heat in the heat exchange to these outlet pipes 16. This construction already shown in P 27 19 634.5, the hot gas of the pre-zones as it were in the short-circuit path, bypassing the aluminum components in the heat exchange directly To extract heat in the direction of the device outlet is shown in FIG. 1 of this additional application for the application shown that the pre-zone is not as shown in FIGS 3 are arranged in the rear part of the exhaust system, but in the front part. Of the This does not change the technological content of the specified statement. In In all three cases there is a direct supply of heat from the heat exchange Pre-zone in the direction of the device outlet, skipping the aluminum parts. In Fig Ur 1 is room 4, the pre-zone that supplies the hot gas to the aluminum parts. That The aluminum component included in the construction of Figure 1 is an extruded one Tube with the gas duct groups 14, 12 and 11 (enumerated from the outside to the inside). In its interior, the gas guide space 11 is usually not made of aluminum manufactured pipe 16 crosses, which at the same time the outlet pipe of the exhaust gas in the free Represents atmosphere. From the partial flow groups 14, the exhaust gas runs over the thermal cooling space 10 through the line 11 and the holes 15 in the cone interior 18, which is with its wall 19 in heat exchange to the hot gas zone 4, namely with very large surface. The amount of heat now fed through the pipe 16 to the outlet relieves the exhaust gas ducts, which have completely or partially aluminum walls.

L e e r s e i t eL e r s e i t e

Claims (1)

Patentanspruch 1. Thermische Abgasführung mit dem aluminiumgefertigten Bauelement eines Hohlkammerringrohres, das in Schalldämpfer oder Kühl strecken der Abgasanlagen von Brennkraftmaschinen integriert ist und durch Rippen in langgctreckte, insbesondere in Wegenstromanordnung laufende Gasfiih-rungsgruppen unterteilt ist, mit dem Merkmal, daß die Außenwandung des Ilohlkammermantels in die freie Atmosphäre abstrahlt, und «em weiteren merkmal, daß die Abgasmenge, welche die erste Gasführung verläßt, vor Eintritt in die nächste Gasführungsstrecke mit Aluminumwand eine thermische Zwischenzone passiert, in welcher sie einen weiteren Wärmeverlust erleidet, dadurch gekennzeichnet, daß innerhalb der zwischen Motorauslaß und erster Beaufschlagung von Aluminiumwandungen gelegenen Abgaseinlaufzone (sog. Vorzone, Figur 1 1/2/4, Figur 2 : 1/2/17, Figur 3 : 1/2/17) Wärmetauschwandung zu einem stromabwärts der erstbeaufschlagten Aluminum-Gasführungsleitungen gelegenen Gerätaustrittsrohr (Figur 2 : 16, Figur 3 : 16) oder dessen Zuführungsleitungen (Figur 1 : 18) vorgesehen ist. Claim 1. Thermal exhaust system with the aluminum-made Component of a hollow chamber ring tube that stretch in the silencer or cooling Exhaust systems of internal combustion engines is integrated and by ribs in elongated, in particular, gas supply groups running in a path flow arrangement are subdivided, with the feature that the outer wall of the Ilohlkammermantels in the free atmosphere emits, and a further feature that the amount of exhaust gas that the first gas guide leaves, before entering the next gas routing section with an aluminum wall, a thermal Intermediate zone happens in which she suffers a further loss of heat, thereby characterized in that within the between the engine outlet and the first application exhaust gas inlet zone located by aluminum walls (so-called pre-zone, figure 1 1/2/4, Figure 2: 1/2/17, Figure 3: 1/2/17) heat exchange wall to a downstream of the first pressurized aluminum gas ducts located device outlet pipe (Fig 2: 16, Figure 3: 16) or its feed lines (Figure 1: 18) are provided is.
DE19772733443 1977-04-28 1977-07-25 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas Withdrawn DE2733443A1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
DE19772733443 DE2733443A1 (en) 1977-05-03 1977-07-25 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE19772747655 DE2747655A1 (en) 1977-07-25 1977-10-24 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
IT22649/78A IT1095302B (en) 1977-04-28 1978-04-24 CONDUCTION SYSTEM FOR GAS APPLIANCES WITH DISCHARGE IN THE FREE ATMOSPHERE, IN PARTICULAR FOR MOTOR DRIVE ELEMENTS
JP4868178A JPS5416041A (en) 1977-04-28 1978-04-24 Multipleewall hollow mold material with blockade body for guiding thermal gas
GB16521/78A GB1603962A (en) 1977-04-28 1978-04-26 Gas discharge apparatus
US05/900,247 US4233812A (en) 1977-04-28 1978-04-26 Gas discharge apparatus
BE187201A BE866483A (en) 1977-04-28 1978-04-27 GAS CONDUCTION DEVICE AND HOLLOW PROFILES FOR ITS REALIZATION
FR7812561A FR2388993A1 (en) 1977-04-28 1978-04-27 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19772719634 DE2719634A1 (en) 1977-05-02 1977-05-03 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE19772733443 DE2733443A1 (en) 1977-05-03 1977-07-25 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

Publications (1)

Publication Number Publication Date
DE2733443A1 true DE2733443A1 (en) 1979-02-08

Family

ID=25771960

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19772733443 Withdrawn DE2733443A1 (en) 1977-04-28 1977-07-25 Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas

Country Status (1)

Country Link
DE (1) DE2733443A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITCR20100011A1 (en) * 2010-04-13 2011-10-14 Michele Parodi SILENCED GAS DRAINAGE DEVICE FOR TWO STROKE BURST MOTORS

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITCR20100011A1 (en) * 2010-04-13 2011-10-14 Michele Parodi SILENCED GAS DRAINAGE DEVICE FOR TWO STROKE BURST MOTORS

Similar Documents

Publication Publication Date Title
DE2547229C2 (en) Air branch device for an axial compressor of a gas turbine engine
DE874680C (en) Nozzle box for gas turbine engines
DE3447717A1 (en) GAS TURBINE SYSTEM
DE2846455C2 (en) Shell and tube heat exchanger with a constant outlet temperature of one of the two media
DE2352965A1 (en) ARRANGEMENT FOR EXHAUST GAS DETOXIFICATION FROM COMBUSTION MACHINES
DE69002283T2 (en) GAS TURBINE ENGINE UNIT.
DE1081768B (en) Device for preventing the formation of ice on an aircraft gas turbine engine with an axial compressor
DE1132002B (en) Preferably designed as an afterburner outlet nozzle for an aircraft engine bundle
DE2733443A1 (en) Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE3903174C2 (en)
DE102016013459A1 (en) Process for changing the temperature of a fluid by means of a shell-and-tube heat exchanger and shell-and-tube heat exchanger
DE874678C (en) Pipe gas heaters, especially for solid fuels, preferably for use in two-stage gas turbine plants
DE2327244A1 (en) BURNER HOUSING AND COOLING STRUCTURE
CH641890A5 (en) KAELTEAGGREGAT.
DE2530198C3 (en) Device for drying gases
DE2747655A1 (en) Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE748857C (en) Cylindrical gas-cooled gas or intermediate cooler, e.g. for charge air from internal combustion engines
DE868806C (en) Gas turbine plant partially working in a cycle
DE2721956A1 (en) Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE2730480A1 (en) Internal combustion engine exhaust system and silencer - uses tubes with multiple bores to cool exhaust gas
DE842348C (en) Steam temperature controller with surface heat exchanger
DE2452418A1 (en) Afterburner for gases exhausted from processing plants - having compactly arranged double heat recuperation equipment
DE2111586C3 (en) Heater for flowing media
DE661558C (en) Device for regulating the room temperature, especially of railroad cars
DE2716458A1 (en) Vehicle engine silencer exhaust gas cooler - has integrated gas conversion unit esp. thermal reactor

Legal Events

Date Code Title Description
8130 Withdrawal